View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53566U 26145.51682528 +.00000000 +00000-0 +12701-4 0 00008
2 53566 53.2124 69.2178 0001124 103.6045 256.5073 15.08839283 09
| Epoch (UTC): | 25 May 2026 12:24:13 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.2178° |
| argument of perigee: | 103.6045° |
| revolutions per day: | 15.08839283 |
| mean anomaly at epoch: | 256.5073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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